CN206756173U - A kind of double air chamber nuclear spin gyroscopes - Google Patents

A kind of double air chamber nuclear spin gyroscopes Download PDF

Info

Publication number
CN206756173U
CN206756173U CN201720655084.1U CN201720655084U CN206756173U CN 206756173 U CN206756173 U CN 206756173U CN 201720655084 U CN201720655084 U CN 201720655084U CN 206756173 U CN206756173 U CN 206756173U
Authority
CN
China
Prior art keywords
laser
air chamber
coil
caused
magnetic
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn - After Issue
Application number
CN201720655084.1U
Other languages
Chinese (zh)
Inventor
舒强
朱明智
汪宝旭
吴文凯
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Engineering Research Institute China Academy of Engineering Physics
Original Assignee
General Engineering Research Institute China Academy of Engineering Physics
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by General Engineering Research Institute China Academy of Engineering Physics filed Critical General Engineering Research Institute China Academy of Engineering Physics
Priority to CN201720655084.1U priority Critical patent/CN206756173U/en
Application granted granted Critical
Publication of CN206756173U publication Critical patent/CN206756173U/en
Withdrawn - After Issue legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Magnetic Resonance Imaging Apparatus (AREA)

Abstract

The utility model discloses a kind of double air chamber nuclear spin gyroscopes, including the first magnetic screen shell, first air chamber, first pumping coil, first main field coil, first laser detector, second magnetic screen shell, second air chamber, second pumping coil, second main field coil, second laser detector, laser, magnetic field generator and signal processor, the second air chamber and the first air chamber are then passed through after the second pumping coil and the first pumping coil are each passed through after laser is divided into two caused by laser, then it is transferred to signal processor after second laser detector and the detection of first laser detector.The utility model is using double air chamber schemes, the polarization FID processes of each air chamber can be controlled alternately, previous short time when so calculating gyro signal all after the FID processes of each air chamber start is carried out, FID signal intensity is higher, signal to noise ratio is improved very well, high sensitivity, continuous angular displacement signal can be obtained compared to single air chamber scheme.

Description

A kind of double air chamber nuclear spin gyroscopes
Technical field
It the utility model is related to a kind of nuclear gyroscope, more particularly to a kind of double air chamber nuclear spin gyroscopes.
Background technology
Gyroscope is the core sensor of inertial navigation system, and its performance will directly determine the navigation accuracy of inertial navigation system.It is high-precision Spend the development experience liquid floated gyroscope using Newton classic mechanics as theoretical foundation, the flexure gyroscope of gyroscope, to Lasergyro, fibre optic gyroscope based on Sagnac (Sagnac) effect, the operation principle and performance of gyroscope occur Earth-shaking change.With the fast development of modern physicses, atom cooling, atom manipulate, the made rapid progress of laser technology, Be born a kind of novel gyroscope i.e. atomic gyroscope using Atomic Physics and quantum mechanics as theoretical foundation again.
Atomic gyroscope is also referred to as nuclear gyroscope or atom nuclear gyroscope, and nuclear spin gyroscope be it is a kind of based on atom from The atomic gyroscope of rotation, the precision level of present laser gyroscope can be reached, the need of tactics class precision Navigation Control can be met Ask, have in miniaturization and low cost and have great advantage.For example the United States Patent (USP) of Patent No. " US4157495 " describes one Atom laser gyroscope of the kind based on nuclear magnetic resonance, intert-gas atoms is produced macroscopic moment using spin-exchange polarization, applied laterally Add a frequency to be equal to the alternating excitation magnetic field of Larmor frequency and maintain nuclear spin precession, the frequency in transversely excited magnetic field need to pass through The feedback of phase or frequency is allowed to the Larmor precession phase consistently equal to observed or frequency;Application No. A kind of micro-structural magnetic resonance gyroscope instrument of the Introduction To Cn Patent of " 201410850412.4 ", its operation principle is the same as the above-mentioned U.S. Patent is identical;German P.Harle (Stuttgart University) et al. describes one kind and is based on nuclear spin and optical pumping Angular transducer, the FID signal using the intert-gas atoms magnetic moment of single air chamber be free induction decay signal extraction angle Spend information.
Above-mentioned traditional nuclear spin gyroscope, the first and second are required for the transversely excited magnetic field of feedback, to phase The precision and real-time of control have high requirements, and control algolithm is complicated, requirement of real-time is high;The third is due to FID signal Decay, signal to noise ratio drastically decline, and the bias stability of measurement sensitivity and angle strongly reduces, so continuous angle can not be realized Degree measurement.
Utility model content
The purpose of this utility model is that to solve the above problems and provides a kind of double air chamber nuclear spin gyroscopes, its FID signal intensity is higher, and signal to noise ratio is improved very well, high sensitivity, can obtain continuous angular displacement signal.
The utility model is achieved through the following technical solutions above-mentioned purpose:
A kind of double air chamber nuclear spin gyroscopes, including the first magnetic screen shell, the first air chamber, the first pumping coil, first Main field coil, first laser detector, the second magnetic screen shell, the second air chamber, the second pumping coil, the second main magnetic field lines Circle, second laser detector, laser, magnetic field generator and signal processor, first air chamber, the first pumping coil It is placed in first main field coil in the first magnetic screen shell, magnetic field and institute caused by the first pumping coil Magnetic direction caused by stating the first main field coil is mutually perpendicular to and can pass through first air chamber, second air chamber, institute State the second pumping coil and second main field coil is placed in the second magnetic screen shell, the second pumping coil Magnetic direction caused by caused magnetic field and second main field coil is mutually perpendicular to and can pass through second air chamber;Institute It is identical with magnetic direction caused by the second pumping coil to state magnetic field caused by the first pumping coil, first main magnetic field lines Magnetic field caused by circle is identical with magnetic direction caused by second main field coil, shape, described the first of size all same The gentle qi of chong channel ascending adversely of intert-gas atoms in air chamber and second air chamber comprising alkali metal atom, for spin-exchange polarization Body, the control output end of the magnetic field generator input with the first pumping coil, first main magnetic field lines respectively The input of the input of circle, the input of the second pumping coil and second main field coil is corresponding to be connected, described Laser caused by laser is divided into two be each passed through first air chamber and second air chamber after be radiated at described respectively The induction end of the induction end of one laser detector and the second laser detector, the signal output of the first laser detector Input of the signal output part of end and the second laser detector respectively with the signal processor is connected.
Specifically, the first laser detector, the second laser detector, the laser, the magnetic field occur Device and the signal processor are placed in outside the first magnetic screen shell and the second magnetic screen shell.
Specifically, the laser can be one and be pump laser, in laser caused by the pump laser Half laser after the half reflection reflection of pump power mirror reflection with half reflection and half transmission function is along the first pumping coil Caused magnetic direction passes through described second through first air chamber or along magnetic direction caused by the second pumping coil Air chamber, second half laser in laser caused by the pump laser after half reflection reflection of pump power mirror transmission is through tool The total reflection reflection of pump power mirror for having total reflection function passes through described along magnetic direction caused by the second pumping coil after reflecting Second air chamber passes through first air chamber, the first laser detector along magnetic direction caused by the first pumping coil It is photodetector with the second laser detector.
As needed, the laser can also be two and respectively pump laser and detecting laser, the pump Half in laser caused by the laser of Pu after the half reflection reflection of pump power mirror reflection with half reflection and half transmission function swashs Magnetic direction caused by light along the first pumping coil is through first air chamber or along caused by the second pumping coil Magnetic direction passes through second air chamber, and it is saturating to pass through the half reflection reflection of pump power mirror in laser caused by the pump laser Second half laser after penetrating produces after the total reflection reflection of pump power mirror reflection with total reflection function along the second pumping coil Raw magnetic direction through second air chamber or passes through first gas along magnetic direction caused by the first pumping coil Room;In laser caused by the detecting laser after with the half reflection of half reflection and half transmission function detection speculum reflection Half laser along simultaneously with first main field coil caused by magnetic caused by magnetic direction and the first pumping coil The vertical direction of field direction through first air chamber or along simultaneously with second main field coil caused by magnetic direction and The vertical direction of magnetic direction caused by the second pumping coil passes through second air chamber, caused by the detecting laser Second half laser in laser after half reflection detection speculum transmission passes through the total reflection detection with total reflection function Along while with caused by magnetic direction caused by second main field coil and the second pumping coil after speculum reflection The vertical direction of magnetic direction through second air chamber or simultaneously with first main field coil caused by magnetic direction and The vertical direction of magnetic direction caused by the first pumping coil passes through first air chamber;Caused by the detecting laser Two parts of laser are each passed through the sense that the first laser detector is radiated at after first air chamber and second air chamber The induction end of second laser detector described in Ying Duanhe, the first laser detector and the second laser detector are difference Fraction polarization detector.
The beneficial effects of the utility model are:
The utility model can control the polarization-FID processes of each air chamber alternately, so using double air chamber schemes Previous short time when calculating gyro signal all after the FID processes of each air chamber start is carried out, and FID signal intensity is higher, Signal to noise ratio is improved very well, high sensitivity, and continuous angular displacement signal can be obtained compared to single air chamber scheme.
Brief description of the drawings
Fig. 1 is the structural representation of double air chamber nuclear spin gyroscopes described in the utility model embodiment 1;
The magnetic field that Fig. 2 is the first air chamber described in the utility model embodiment 1 and the second air chamber alternant polarization-FID controlled Journey schematic diagram;
Fig. 3 is the structural representation of double air chamber nuclear spin gyroscopes described in the utility model embodiment 2.
Embodiment
With reference to embodiment and accompanying drawing, the utility model is described in further detail:
Embodiment 1:
As shown in figure 1, a kind of double air chamber nuclear spin gyroscopes, including the first magnetic screen shell 7, the first air chamber 1, the first pump Pu coil 5, the first main field coil 3, first laser detector 9, the second magnetic screen shell 8, the second air chamber 2, the second pumping line The 6, second main field coil 4, second laser detector 10, pump laser 11, magnetic field generator 14 and signal processor 15 are enclosed, First air chamber 1, the first pumping coil 5 and the first main field coil 3 are placed in the first magnetic screen shell 7, the second air chamber 2, Two pumping coils 6 and the second main field coil 4 are placed in the second magnetic screen shell 8, first laser detector 9, second laser Detector 10, pump laser 11, magnetic field generator 14 and signal processor 15 are placed in the first magnetic screen shell 7 and the second magnetic Shield outside shell 8;Magnetic direction caused by magnetic field caused by first pumping coil 5 and the first main field coil 3 be mutually perpendicular to and The first air chamber 1 can be passed through, magnetic direction caused by magnetic field caused by the second pumping coil 6 and the second main field coil 4 is mutual Vertically and it can pass through the second air chamber 2;Magnetic field caused by first pumping coil 5 and magnetic direction caused by the second pumping coil 6 Identical, magnetic field is identical with magnetic direction caused by the second main field coil 4 caused by the first main field coil 3, and shape, size are equal In identical the first air chamber 1 and the second air chamber 2 comprising alkali metal atom, the intert-gas atoms for spin-exchange polarization and Buffer gas, the control output end of magnetic field generator 14 input with the first pumping coil 5, the first main field coil 3 respectively Input, the second pumping coil 6 input and the second main field coil 4 input it is corresponding connect, pump laser 11 Half laser in caused laser after the half reflection reflection of pump power mirror 13 with half reflection and half transmission function reflects is along the Magnetic direction caused by two pumping coils 6 passes through the second air chamber 2, is then radiated at the induction end of second laser detector 10, pump Second half laser in laser caused by Pu laser 11 after the transmission of half reflection reflection of pump power mirror 13, which passes through, has total reflection work( After the reflection of total reflection reflection of pump power mirror 12 of energy the first air chamber 1, Ran Houzhao is passed through along magnetic direction caused by the first pumping coil 4 Penetrate the induction end in first laser detector 9, the signal output part of first laser detector 9 and the letter of second laser detector 10 Number input of the output end respectively with signal processor 15 is connected;First laser detector 9 and second laser detector 10 are Photodetector;Half reflection reflection of pump power mirror 13 is a kind of spectroscope.Explanation:The order that above-mentioned pumping laser is divided into two also may be used With on the contrary, can first along magnetic direction caused by the first pumping coil 5 pass through the first air chamber 1 after be radiated at first laser detection The induction end of device 9, irradiated after then second half laser is again along magnetic direction caused by the second pumping coil 6 through the second air chamber 2 In the induction end of second laser detector 10, such case and the outside for being located proximate to the first air chamber 1 of pump laser 11 Structure is corresponding.
In said structure, if the three-dimensional coordinate formed with x-axis, y-axis, z-axis represents direction, the He of the first pumping coil 5 Magnetic direction caused by second pumping coil 6 is x-axis direction, magnetic caused by the first main field coil 3 and the second main field coil 4 Field direction is z-axis direction.
In said structure, preferred structure is:First air chamber 1 and the heat-resisting glass that the second air chamber 2 is the length of side about 2~10mm Cube made of glass or the suitable glass envelope of size;Contain number mbar's in two air chambers129Xe, number mg metal87Rb steams Vapour, simultaneously the buffer N containing tens mbar2;In order to improve gyro resolution ratio, reduce the interference of external magnetic field, Xe in air chamber Atom can use two kinds of isotope atoms, such as129Xe and131Xe;After air chamber structure part machines, clean processing must be carried out, Then, plated film (such as rubidium hydride or Parylene) processing is carried out to air chamber inner surface as needed;First magnetic screen shell 7 and second The material of magnetic screen shell 8 uses sandwich construction, and innermost layer uses high permeability materials (mu-metal), to provide high magnetic screen Coefficient, outer layer use low permeability magnetic material, to make it have higher diamagnetic saturation intensity.
In order to make it easy to understand, the preferred control method that double air chamber nuclear spin gyroscopes above-mentioned to the utility model use below It is illustrated, but following methods are not unique methods, nor protection object of the present utility model.
As depicted in figs. 1 and 2, the preferred control method that double air chamber nuclear spin gyroscopes described in the present embodiment use, including Following steps:
(1) control the first pumping coil 5 to produce magnetic field by magnetic field generator 14, open pump laser 11, the first air chamber 1 Intert-gas atoms be polarized under corresponding pump light by the spin exohange collision with alkali metal atom, break after the completion of polarization Open the power supply of the first pumping coil 5;
(2) the first main field coil 3 is controlled to produce magnetic field, the indifferent gas to be polarized in the first air chamber 1 by magnetic field generator 14 Body atom surrounds corresponding main field and does Larmor precession;
(3) first laser detector 9 detects the FID signal through the first air chamber 1 and is transferred to signal processor 15 and calculates Angular displacement;
(4) the second pumping coil 6 is controlled to produce magnetic field by magnetic field generator 14, the intert-gas atoms of the second air chamber 2 exist It is polarized under corresponding pump light by the spin exohange collision with alkali metal atom, the second pumping coil 6 is disconnected after the completion of polarization Power supply;
(5) the second main field coil 4 is controlled to produce magnetic field, the indifferent gas to be polarized in the second air chamber 2 by magnetic field generator 14 Body atom surrounds corresponding main field and does Larmor precession;
(6) second laser detector 10 detects the FID signal through the second air chamber 2 and is transferred to signal processor 15 and calculates Angular displacement;
(7) repeat step (1)-step (6), the phase offset that signal processor 15 is resolved using two-way FID signal are spelled Connect to obtain continuous angular displacement signal, specifically, when gyroscope rotates around z-axis, gyro angle position can be introduced in this phase angle Shifting signal, by compared with reference clock signal, obtaining continuous angular displacement signal.
Embodiment 2:
The present embodiment is the deformation carried out on the basis of embodiment 1, and its difference is:
As shown in figure 3, the laser is two and respectively pump laser 11 and detecting laser 20, pumping laser Half laser in laser caused by device 11 after the half reflection reflection of pump power mirror 13 with half reflection and half transmission function reflects 2 second air chambers are passed through along magnetic direction caused by the second pumping coil 6, pass through half reflection in laser caused by pump laser 11 Reflection of pump power mirror 13 transmit after second half laser pass through the reflection of total reflection reflection of pump power mirror 12 with total reflection function after along the Magnetic direction caused by one pumping coil 5 passes through the first air chamber 1;By having half reflection in laser caused by detecting laser 20 Half transmitting function half reflection detection speculum 19 reflect after half laser along simultaneously with the second main field coil 4 caused by magnetic The vertical direction JizZhou directions of magnetic direction caused by field direction and the second pumping coil 6 pass through the second air chamber 2, exploring laser light Second half laser in laser caused by device 20 after half reflection detection speculum 19 transmits is passed through with the complete of total reflection function Reflection detection speculum 18 reflect after along simultaneously with the first main field coil 3 caused by magnetic direction and the first pumping coil 5 produce The vertical direction JizZhou directions of raw magnetic direction pass through the first air chamber 1;Two parts of laser caused by detecting laser 20 point The induction end and the second differential type of the first differential type polarization detector 16 Chuan Guo not be radiated at after the first air chamber 1 and the second air chamber 2 The induction end of polarization detector 17, the signal output part of the first differential type polarization detector 16 and the second differential type polarization detector Input of 17 signal output part respectively with signal processor 15 is connected.
Comparison diagram 3 and Fig. 1 understands that the architectural difference of the present embodiment compared with Example 1 is:The present embodiment is in embodiment Detecting laser 20, half reflection detection speculum 19 and total reflection detection speculum 18 are added on the basis of 1, and it is poor with first The differential type polarization detector 17 of fraction polarization detector 16 and second instead of the first laser detector 9 and second of embodiment 1 The two photodetectors of laser detector 10.
Correspondingly, the preferred control method of the present embodiment is also corresponded to and changed, and the control method of the present embodiment is:
(1) control the first pumping coil 5 to produce magnetic field by magnetic field generator 14, open pump laser 11 and exploring laser light Device 20, the intert-gas atoms of the first air chamber 1 pass through the spin-exchange with alkali metal atom under corresponding pump light and detection light Collision is polarized, and the power supply of the first pumping coil 5 is disconnected after the completion of polarization;
(2) the first main field coil 3 is controlled to produce magnetic field, the indifferent gas to be polarized in the first air chamber 1 by magnetic field generator 14 Body atom surrounds corresponding main field and does Larmor precession;
(3) first differential type polarization detectors 16 detection detection light passes through the FID signal formed after the first air chamber 1 and transmission Polarization is calculated to the anglec of rotation to signal processor 15;
(4) the second pumping coil 6 is controlled to produce magnetic field by magnetic field generator 14, the intert-gas atoms of the second air chamber 2 exist It is polarized under corresponding pump light and detection light by the spin exohange collision with alkali metal atom, the second pump is disconnected after the completion of polarization The power supply of Pu coil 6;
(5) the second main field coil 4 is controlled to produce magnetic field, the indifferent gas to be polarized in the second air chamber 2 by magnetic field generator 14 Body atom surrounds corresponding main field and does Larmor precession;
(6) second differential type polarization detectors 17 detection detection light passes through the FID signal formed after the second air chamber 2 and transmission Polarization is calculated to the anglec of rotation to signal processor 15;
(7) repeat step (1)-step (6), signal processor 15 is using the polarization that two-way FID signal resolves to rotation Angle, which is spliced, continuously to be polarized to rotary angle signal.
Above-described embodiment is preferred embodiment of the present utility model, is not the limit to technical solutions of the utility model System, as long as the technical scheme that can be realized without creative work on the basis of above-described embodiment, is regarded as falling into In the rights protection scope of the utility model patent.

Claims (4)

  1. A kind of 1. double air chamber nuclear spin gyroscopes, it is characterised in that:Including the first magnetic screen shell, the first air chamber, the first pumping Coil, the first main field coil, first laser detector, the second magnetic screen shell, the second air chamber, the second pumping coil, second Main field coil, second laser detector, laser, magnetic field generator and signal processor, first air chamber, described first Pumping coil and first main field coil are placed in the first magnetic screen shell, caused by the first pumping coil Magnetic direction caused by magnetic field and first main field coil is mutually perpendicular to and can pass through first air chamber, and described second Air chamber, the second pumping coil and second main field coil are placed in the second magnetic screen shell, and described second Magnetic direction caused by magnetic field caused by pumping coil and second main field coil is mutually perpendicular to and can be through described the Two air chambers;Magnetic field is identical with magnetic direction caused by the second pumping coil caused by the first pumping coil, and described Magnetic field caused by one main field coil is identical with magnetic direction caused by second main field coil, shape, size all same First air chamber and second air chamber in comprising alkali metal atom, the intert-gas atoms for spin-exchange polarization And buffer gas, the control output end of the magnetic field generator input with the first pumping coil, described first respectively The input of the input of main field coil, the input of the second pumping coil and second main field coil correspondingly connects Connect, laser caused by the laser is divided into two be each passed through first air chamber and second air chamber after be radiated at respectively The induction end of the induction end of the first laser detector and the second laser detector, the letter of the first laser detector Input of the signal output part of number output end and the second laser detector respectively with the signal processor is connected.
  2. 2. double air chamber nuclear spin gyroscopes according to claim 1, it is characterised in that:The first laser detector, institute State second laser detector, the laser, the magnetic field generator and the signal processor and be placed in first magnetic cup Cover outside shell and the second magnetic screen shell.
  3. 3. double air chamber nuclear spin gyroscopes according to claim 1 or 2, it is characterised in that:The laser be one and It is anti-to pass through the half reflection pumping with half reflection and half transmission function for pump laser, in laser caused by the pump laser Magnetic direction is through first air chamber or along described caused by the half laser along the first pumping coil penetrated after mirror reflection Magnetic direction caused by second pumping coil passes through second air chamber, passes through in laser caused by the pump laser described Second half laser after the transmission of half reflection reflection of pump power mirror is through with edge after being totally reflected the total reflection reflection of pump power mirror reflection of function Magnetic direction caused by the second pumping coil is through second air chamber or along magnetic field caused by the first pumping coil Direction passes through first air chamber, and the first laser detector and the second laser detector are photodetector.
  4. 4. double air chamber nuclear spin gyroscopes according to claim 1 or 2, it is characterised in that:The laser be two and Respectively pump laser and detecting laser, by having half reflection and half transmission work(in laser caused by the pump laser Magnetic direction is described in caused by half laser along the first pumping coil after the half reflection reflection of pump power mirror reflection of energy First air chamber passes through second air chamber along magnetic direction caused by the second pumping coil, and the pump laser produces Laser in by the half reflection reflection of pump power mirror transmission after second half laser pass through with total reflection function total reflection pump Along magnetic direction caused by the second pumping coil through second air chamber or along first pump after the reflection of Pu speculum Magnetic direction caused by the coil of Pu passes through first air chamber;By having half reflection in laser caused by the detecting laser Half laser after the half reflection detection speculum reflection of half transmitting function is along while with caused by first main field coil The vertical direction of magnetic direction caused by magnetic direction and the first pumping coil through first air chamber or along simultaneously with Wear in the vertical direction of magnetic direction caused by magnetic direction caused by second main field coil and the second pumping coil Second air chamber is crossed, is detected in laser caused by the detecting laser by the half reflection another after speculum transmits Half laser produces on edge with second main field coil simultaneously after the total reflection detection speculum reflection with total reflection function Magnetic direction and the second pumping coil caused by the vertical direction of magnetic direction through second air chamber or simultaneously with Wear in the vertical direction of magnetic direction caused by magnetic direction caused by first main field coil and the first pumping coil Cross first air chamber;Two parts of laser caused by the detecting laser are each passed through first air chamber and described second The induction end of the first laser detector and the induction end of the second laser detector are radiated at after air chamber, described first swashs Photo-detector and the second laser detector are differential type polarization detector.
CN201720655084.1U 2017-06-07 2017-06-07 A kind of double air chamber nuclear spin gyroscopes Withdrawn - After Issue CN206756173U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720655084.1U CN206756173U (en) 2017-06-07 2017-06-07 A kind of double air chamber nuclear spin gyroscopes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720655084.1U CN206756173U (en) 2017-06-07 2017-06-07 A kind of double air chamber nuclear spin gyroscopes

Publications (1)

Publication Number Publication Date
CN206756173U true CN206756173U (en) 2017-12-15

Family

ID=60622400

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201720655084.1U Withdrawn - After Issue CN206756173U (en) 2017-06-07 2017-06-07 A kind of double air chamber nuclear spin gyroscopes

Country Status (1)

Country Link
CN (1) CN206756173U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107063226A (en) * 2017-06-07 2017-08-18 中国工程物理研究院总体工程研究所 A kind of pair of air chamber nuclear spin gyroscope and its control method
WO2020119642A1 (en) * 2018-12-10 2020-06-18 中科知影(北京)科技有限公司 Multi-channel atomic magnetic detector

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107063226A (en) * 2017-06-07 2017-08-18 中国工程物理研究院总体工程研究所 A kind of pair of air chamber nuclear spin gyroscope and its control method
CN107063226B (en) * 2017-06-07 2023-05-02 中国工程物理研究院总体工程研究所 Double-air-chamber nuclear spin gyroscope and control method thereof
WO2020119642A1 (en) * 2018-12-10 2020-06-18 中科知影(北京)科技有限公司 Multi-channel atomic magnetic detector

Similar Documents

Publication Publication Date Title
CN107063226A (en) A kind of pair of air chamber nuclear spin gyroscope and its control method
CN108508382B (en) Three-dimensional gradient magnetic field measuring device based on SERF atomic spin effect
JP5232837B2 (en) Nuclear magnetic resonance gyroscope system, three-axis gyroscope system, and method for determining a rotation angle about a sensitive axis of a nuclear magnetic resonance gyroscope system
US4157495A (en) Nuclear magnetic resonance gyro
CN103438877B (en) A kind of inertia based on SERF atomic spin effect and magnetic field integral measurement method
CN105588555B (en) A kind of passive method for shielding of master
CN102914298B (en) Fullerene molecular gyroscope
CN106017451A (en) High-precision measurement method for magnetic field compensation inertial angular rate based on of SERF (spin-exchange relaxation free) atomic device
CN104634339A (en) Nuclear magnetic resonance gyroscope based on wide spectrum laser pumping
CN110568382B (en) Double-pumping light beam three-axis atomic vector magnetic field measuring device based on SERF
CN104697512A (en) Diamond color center gyroscope based on Aharonov-Anandan geometric phase and angular velocity measuring method
CN109541500B (en) Co-magnetometer based on alkali metal atom hyperfine energy level Zeeman splitting
JP2014504729A (en) Magnetic field error correction of gyroscope system
CN206756173U (en) A kind of double air chamber nuclear spin gyroscopes
CN203519846U (en) Vertical gravity gradient measurement sensor based on atomic interference effects
CN203759269U (en) Combined inertia sensor based on multi-component atom interferometer
CN103604429A (en) Synchronous atom inertia and magnetic field measurement device based on K-Rb-Ne
CN105674972A (en) Miniature combined uniaxial cold atom inertial sensor and measuring method thereof
JP2008544284A (en) Device and method for integrating continuous and discontinuous inertial instrument measurements in navigation systems.
JP2016128817A (en) Ratiometric nuclear magnetic resonance (NMR) gyroscope system
CN104280023B (en) A kind of coherent layout Trapping of Atoms clock and nuclear magnetic resonance atomic gyroscope integral system
CN103528580A (en) Method for measuring rotating angle of aircraft based on nuclear magnetic resonance
CN111060089B (en) High-sensitivity nuclear spin precession detection method based on electron spin magnetic resonance difference
CN110068320B (en) Zero-bias self-calibration atomic gyroscope
CN109443337A (en) A kind of Position Fixing Navigation System and method based on NV colour center in diamond

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
AV01 Patent right actively abandoned
AV01 Patent right actively abandoned
AV01 Patent right actively abandoned

Granted publication date: 20171215

Effective date of abandoning: 20230502

AV01 Patent right actively abandoned

Granted publication date: 20171215

Effective date of abandoning: 20230502